The invention relates to the technical field of aircraft accessory design, in particular to an undercarriage stay bar unlocking actuator of an air spring, which comprises a controller, a motor driver, a brushless direct current motor, a hydraulic pump, an overflow valve, a shuttle valve, an oil injection one-way valve, an exhaust one-way valve, an exhaust one-way valve and an actuating cylinder, the air cavity piston divides the upper part of the actuating cylinder into an air spring and an oil tank, a piston rod is arranged in the actuating cylinder and divides the lower part of the actuating cylinder into an extension cavity and a retraction cavity, and the oil tank is communicated with the extension cavity through an oil tank bushing; the controller, the motor driver, the motor and the hydraulic pump are electrically connected in sequence. An inlet of the hydraulic pump is connected with the oil injection one-way valve, the exhaust one-way valve and the extending cavity through oil ways in sequence. An outlet of the hydraulic pump is sequentially connected with an overflow valve, a shuttle valve and a retraction cavity of the actuator cylinder through oil ways, the overflow valve is connected with an oil-injection one-way valve oil way, and the shuttle valve is connected with an exhaust one-way valve oil way through a damping hole.
本申请涉及飞机附件设计技术领域,具体涉及一种空气弹簧的起落架撑杆解锁作动器,包括控制器、电机驱动器、无刷直流电机、液压泵、溢流阀、梭阀、注油单向阀、排气单向阀、排气单向阀、作动筒,作动筒内部设置气腔活塞,气腔活塞将作动筒上部分为空气弹簧和油箱,作动筒内部设置活塞杆,活塞杆将作动筒下部分为伸出腔和缩回腔,油箱与伸出腔通过油箱衬套相连通;所述的控制器、电机驱动器、电机、液压泵依次电气连接,液压泵进口依次通过油路连接注油单向阀、排气单向阀、伸出腔;液压泵出口通过油路依次连接溢流阀、梭阀、作动筒的缩回腔,溢流阀与注油单向阀油路连接,梭阀通过阻尼孔与排气单向阀油路连接。
Undercarriage stay bar unlocking actuator of air spring
一种空气弹簧的起落架撑杆解锁作动器
2023-03-21
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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